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Adrian L. R. Thomas

Researcher at University of Oxford

Publications -  56
Citations -  6364

Adrian L. R. Thomas is an academic researcher from University of Oxford. The author has contributed to research in topics: Wing & Vortex. The author has an hindex of 29, co-authored 56 publications receiving 5803 citations. Previous affiliations of Adrian L. R. Thomas include University of Cambridge.

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Leading-edge vortices in insect flight

TL;DR: In this article, the authors visualized the airflow around the wings of the hawkmoth Manduca sexta and a 'hovering' large mechanical model, and found an intense leading-edge vortex was found on the downstroke, of sufficient strength to explain the high-lift forces.
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Flying and swimming animals cruise at a Strouhal number tuned for high power efficiency

TL;DR: Tuning cruise kinematics to optimize St seems to be a general principle of oscillatory lift-based propulsion of swimming and flying animals.
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Details of Insect Wing Design and Deformation Enhance Aerodynamic Function and Flight Efficiency

TL;DR: The full-fidelity model achieved greater power economy than the uncambered model, which performed better than the untwisted model, showing that the details of insect wing topography and deformation are important aerodynamically.
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Unconventional lift-generating mechanisms in free-flying butterflies.

TL;DR: Train red admiral butterflies to fly freely to and from artificial flowers in a wind tunnel, and use high-resolution, smoke-wire flow visualizations to obtain qualitative, high-speed digital images of the air flow around their wings, show that free-flying butterflies use a variety of unconventional aerodynamic mechanisms to generate force.
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Dragonfly flight: free-flight and tethered flow visualizations reveal a diverse array of unsteady lift-generating mechanisms, controlled primarily via angle of attack.

TL;DR: It appears that stability of the LEV is achieved by a general mechanism whereby flapping kinematics are configured so that a LEV would be expected to form naturally over the wing and remain attached for the duration of the stroke, however, the actual formation and shed is controlled by wing angle of attack.